MARC Record from marc_columbia

LEADER: 03202cam a2200709 i 4500
001 11608450
005 20221112224133.0
006 m o d
007 cr cnu---unuuu
008 150825s1952 dcua otb f000 0 eng d
035 $a(OCoLC)ocn919140207
035 $a(NNC)11608450
040 $aKNOVL$beng$erda$epn$cKNOVL$dZCU$dUAB$dDKU$dOCLCQ$dCEF$dRRP$dYOU$dS2H$dOCLCO$dCOP
020 $a9781680156249$qelectronic bk.
020 $a1680156241$qelectronic bk.
035 $a(OCoLC)919140207
050 4 $aTA660.P6
082 04 $a624.17765$223
086 0 $aY 3.N 21/5:6/2679
088 $aNACA-TN-2679
049 $aZCUA
100 1 $aSeide, Paul,$eauthor.
245 14 $aThe stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /$cPaul Seide.
264 1 $aWashington, D.C. :$bNational Advisory Committee for Aeronautics,$c1952.
300 $a1 online resource (30 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aNational Advisory Committee for Aeronautics ;$v2679
500 $a"Langley Aeronautical Laboratory.”
500 $aDate of issue: April 1952.
500 $aReport no. NACA-TN-2679.
520 3 $aA theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.
588 0 $aPrint version record.
504 $aIncludes bibliographical references (page 19)
650 0 $aPlates (Engineering)
650 0 $aSandwich construction.
650 0 $aLoads (Mechanics)
650 0 $aBuckling (Mechanics)
650 0 $aElasticity.
650 6 $aPlaques (Ingénierie)
650 6 $aConstruction sandwich.
650 6 $aCharges.
650 6 $aFlambage (Résistance des matériaux)
650 6 $aÉlasticité.
650 7 $awarping.$2aat
650 7 $abuckling.$2aat
650 7 $aelasticity.$2aat
650 7 $amodulus of elasticity.$2aat
650 7 $aBuckling (Mechanics)$2fast$0(OCoLC)fst00840001
650 7 $aElasticity.$2fast$0(OCoLC)fst00904211
650 7 $aLoads (Mechanics)$2fast$0(OCoLC)fst01739107
650 7 $aPlates (Engineering)$2fast$0(OCoLC)fst01066785
650 7 $aSandwich construction.$2fast$0(OCoLC)fst01104954
655 0 $aElectronic books.
655 4 $aElectronic books.
710 2 $aLangley Aeronautical Laboratory.
710 1 $aUnited States.$bNational Advisory Committee for Aeronautics.
776 08 $iPrint version:$aSeide, Paul.$tStability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges$w(OCoLC)667231146
830 0 $aTechnical note (United States. National Advisory Committee for Aeronautics) ;$vno. 2679.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio11608450$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS